On Mon, 3 Jul 2006, Maik Justus wrote: >> We could on the other hand let the model designer set and tweak the >> fuselage Cd manually in the config file. >> > That would be the easier way. Maybe it make sense to look, which results > the solver get for different airplanes.
...faking a wing from rotor data and let ::solver() chew on it perhaps? (I have a rough idea of what drag the chinook fuselage has; this can be derived from cruise pitch and the algorithm for the LCT. But that's not the general solution.) Or translate the rotor equations to jsbsim -- ? Using Tomcat but need to do more? Need to support web services, security? Get stuff done quickly with pre-integrated technology to make your job easier Download IBM WebSphere Application Server v.1.0.1 based on Apache Geronimo http://sel.as-us.falkag.net/sel?cmd=lnk&kid=120709&bid=263057&dat=121642 _______________________________________________ Flightgear-devel mailing list [email protected] https://lists.sourceforge.net/lists/listinfo/flightgear-devel
